Oscillatory aerodynamic forces for a pitching aircraft

Authors

  • R. R. Aggarwal Office Of The D.C.S.O. (Air), New Delhi

DOI:

https://doi.org/10.14429/dsj.11.6789

Keywords:

Bending-torsion, Aerodynamic strip, Oscillations

Abstract

Chordwise aerodynamic strip derivatives for the swept back wing having bending-torsion degrees of freedom as modified by the aircraft simple harmonic pitching oscillations have been calculated.

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Published

2014-03-25

How to Cite

Aggarwal, R. R. (2014). Oscillatory aerodynamic forces for a pitching aircraft. Defence Science Journal, 11(1), 12–14. https://doi.org/10.14429/dsj.11.6789

Issue

Vol. 11 No. 1

Section

Research Papers

License

 Where otherwise noted, the Articles on this site are licensed under Creative Commons License: CC Attribution-Noncommercial-No Derivative Works 2.5 India

 

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